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    Vorticity Modeling of Blade Wakes behind Isolated Annular Blade-Rows: Induced Disturbances in Swirling Flows 

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002:;page 279
    Author(s): C. S. Tan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A general analysis is proposed for studying the fluid-mechanical behavior of blade wakes from an annular blade-row in highly swirling flow. The coupling between the centrifugal force and the ...
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    Control of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001:;page 97
    Author(s): T. Valkov; C. S. Tan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A computational approach, based on a spectral-element Navier–Stokes solver, has been applied to the study of the unsteady flow arising from wake–stator interaction. Direct, as well as turbulence-model ...
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    Effect of Blade Passage Surface Heat Extraction on Axial Compressor Performance 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003:;page 457
    Author(s): P. N. Shah; C. S. Tan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Axial compressor performance with heat extraction via blade passage surfaces (compressor cooling) is compared to its adiabatic counterpart, using computational experiments and mean line modeling. ...
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    Effect of Upstream Rotor Vortical Disturbances on the Time-Averaged Performance of Axial Compressor Stators: Part 1—Framework of Technical Approach and Wake–Stator Blade Interactions 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003:;page 377
    Author(s): T. V. Valkov; C. S. Tan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a two-part paper, key computed results from a set of first-of-a-kind numerical simulations on the unsteady interaction of axial compressor stators with upstream rotor wakes and tip leakage ...
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    Effect of Upstream Rotor Vortical Disturbances on the Time-Averaged Performance of Axial Compressor Stators: Part 2—Rotor Tip Vortex/Streamwise Vortex–Stator Blade Interactions 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003:;page 387
    Author(s): T. V. Valkov; C. S. Tan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a two-part paper, key computed results from a set of first-of-a-kind numerical simulations on the unsteady interaction of axial compressor stator with upstream rotor wakes and tip leakage ...
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    Surface Static Pressures in an Inlet Vortex Flow Field 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 387
    Author(s): W. Liu; E. M. Greitzer; C. S. Tan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation of the three-dimensional flow field associated with an inlet vortex is reported. The specific configuration investigated is an inlet, in proximity to a ground plane, ...
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    Aerodynamic Design of Turbomachinery Blading in Three-Dimensional Flow: An Application to Radial Inflow Turbines 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 602
    Author(s): Y. L. Yang; C. S. Tan; W. R. Hawthorne
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A computational method based on a theory for turbomachinery blading design in three-dimensional inviscid flow is applied to a parametric design study of a radial inflow turbine wheel. As the ...
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    A Design Study of Radial Inflow Turbines With Splitter Blades in Three-Dimensional Flow 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 353
    Author(s): W. D. Tjokroaminata; C. S. Tan; W. R. Hawthorne
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An inverse design technique to design turbomachinery blading with splitter blades in three-dimensional flow is developed. It is based on the use of Clebsch transformation, which allows the ...
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    Impeller–Diffuser Interaction in a Centrifugal Compressor 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 004:;page 777
    Author(s): Y. K. P. Shum; N. A. Cumpsty; C. S. Tan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A study has been conducted, using an unsteady three-dimensional Reynolds-averaged Navier–Stokes simulation, to define the effect of impeller–diffuser interaction on the performance of a centrifugal ...
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    Aerodynamic Response of Turbomachinery Blade Rows to Convecting Density Wakes 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 002:;page 269
    Author(s): H. S. Wijesinghe; C. S. Tan; E. E. Covert
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A two-dimensional computational study was conducted to characterize the density wake induced force and moment fluctuations on a compressor blade row. The flow simulations indicate unsteady blade ...
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